US5006298A - Method of producing a badminton racket frame - Google Patents
Method of producing a badminton racket frame Download PDFInfo
- Publication number
- US5006298A US5006298A US07/545,207 US54520790A US5006298A US 5006298 A US5006298 A US 5006298A US 54520790 A US54520790 A US 54520790A US 5006298 A US5006298 A US 5006298A
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- mold cavity
- racket frame
- badminton racket
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- 238000000034 method Methods 0.000 title claims abstract description 27
- 239000000463 material Substances 0.000 claims abstract description 34
- 239000002904 solvent Substances 0.000 claims abstract description 28
- 239000000835 fiber Substances 0.000 claims abstract description 24
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 20
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 20
- 239000010439 graphite Substances 0.000 claims abstract description 20
- 239000002131 composite material Substances 0.000 claims abstract description 15
- 238000010438 heat treatment Methods 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000002347 injection Methods 0.000 description 4
- 239000007924 injection Substances 0.000 description 4
- YMWUJEATGCHHMB-UHFFFAOYSA-N Dichloromethane Chemical compound ClCCl YMWUJEATGCHHMB-UHFFFAOYSA-N 0.000 description 3
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 101100492805 Caenorhabditis elegans atm-1 gene Proteins 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 239000004088 foaming agent Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- WSLDOOZREJYCGB-UHFFFAOYSA-N 1,2-Dichloroethane Chemical compound ClCCCl WSLDOOZREJYCGB-UHFFFAOYSA-N 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000002498 deadly effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000011342 resin composition Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/46—Component parts, details or accessories; Auxiliary operations characterised by using particular environment or blow fluids other than air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/52—Sports equipment ; Games; Articles for amusement; Toys
- B29L2031/5245—Rackets
Definitions
- the present invention relates to a method, and more particularly to a method of producing a badminton racket frame.
- the first method employs a foamable material.
- the racket comprises a core which includes a foamable material or a foamable resin composition.
- U.S. Pat. No. 4,129,634 to Cecka et al. discloses a method for producing a racket frame which has a strip shaped foamable plastic core disposed therein.
- the strip of foamable material is maintained within a seamless sleeve made of a thin, flexible cellulosic film which is disposed in an outer shell forming the racket frame.
- the outer shell is disposed in a mold cavity.
- the foamable material is caused to expand and to generate pressure within the mold cavity and thereby provide intimate bonding of the core to the shell.
- the powder of foaming agent is blended into or added to the plastics carrier in order to form a strip of foamable material.
- the powder of foaming agent can not be blended evenly in the plastics carrier so that the strip of foamable material has a limited uniformity and may not be expanded or inflated uniformly or evenly.
- the racket frame which is made by the above-mentioned method with a core disposed therein has a weight heavier than the hollow racket frames.
- the second method is an air injection method which employs a pressurized air injected into the racket frame.
- This is the most popular method used today to manufacture both badminton racket and tennis racket.
- the composite structure of the tennis racket frame 20 includes a plurality of layers, each made of a sheet of composite fibers, unidirectionally oriented and resin-impregnated.
- the tennis racket frame 20 has a fluent and smooth passage 21 or hollow interior formed therein and has no sharp angles formed therein so that the pressurized air can be easily injected into the passage 21 of the racket frame 20 from one end of the passage 21. Therefore, the air injection method is suitable for manufacturing tennis racket frames.
- the composite structure of the badminton racket frame comprises a shell 10 including a plurality of layers, each made of a sheet of composite fibers, unidirectionally oriented and resin-impregnated.
- the shell 10 includes a head section 11 and a handle shaft 12 with a passage 14 formed therethrough. One end 15 of the shell 10 is closed. A sharp angle exists between the head section 11 and the handle shaft 12 or in the so called T-joint area.
- a pressurized air is continuously injected into the passage 14 from the free end of the handle shaft 12 in order to expand the shell 10 which is arranged within a mold cavity.
- the pressurized air is jammed or obstructed in the sharp angle portion of the T-joint area, and may not flow through this portion swiftly.
- the head section 11 inflates and the closed end 15 has a tendency to extend toward and to press the passage 14 of the shell 10, particularly the sharp angle area so that the angle area will further be obstructed. Therefore, because of the two deadly problems as mentioned above, about 25% of the products made by this method are rejected products and are unacceptable.
- a compressor or the like is required to produce and to provide the pressurized air.
- the present invention has arisen to solve the afore-described disadvantages of the conventional method for producing badminton racket frames.
- the primary objective of the present invention is to provide a method of producing a badminton racket frame which has an evaporable solvent disposed therein in order to generate a pressure within the racket frame so that the racket frame can be formed uniformly and homogeneously.
- a method of producing a badminton racket frame which includes preparing a mold cavity shaped in the form of a badminton racket frame having a head section and a handle shaft. A number of layers of unidirectionally oriented resin-impregnated graphite fibers are wrapped so as to form a shell shaped in the form of the sections. Solvent material is inserted into the shell and the ends of the shell are closed. The wrapped shell is arranged within the mold cavity. The solvent material is heated to cause expansion and to generate pressure within the mold cavity so as to press against the layers of graphite fibers and thereby provide intimate bonding of the layers. The shell is removed as an integral composite badminton racket frame.
- FIG. 1 is a schematic view of a badminton racket frame made by a method in accordance with the present invention
- FIG. 2 is an enlarged cross sectional view showing the composite structure of the badminton racket frame which has a plurality of successive layers serially exposed;
- FIG. 3 is an enlarged view of a portion of the unidirectionally oriented resin-impregnated graphite fiber structure of the badminton racket frame, with successive layers serially exposed;
- FIG. 4 is a schematic view illustrating the compositions of a strip of a foamable material
- FIG. 5 is a schematic view of a tennis racket frame made by a conventional air injection method.
- FIG. 6 is a schematic view of a badminton racket frame made by a conventional air injection method.
- the badminton racket frame in accordance with the present invention comprises a head section 31 and a handle shaft 32 with a grip affixed to the lower end of the handle shaft 32.
- the structure of the racket frame is generally a shell comprising a plurality of layers 30, each made of a sheet of a so-called prepreg of composite material, or a unidirectionally oriented and resin-impregnated composite material, such as graphite fiber, boron fiber or glass fiber etc., in which most of the racket frames are made of graphite fibers. It is preferable that every two adjacent layers 30 are arranged at predetermined or suitable angles to each other, as shown in FIG. 3.
- the graphite fibers used to make the graphite fiber sheets comprises yarns containing hundreds, or thousands, of individual filaments, as is known in the art.
- the composite structure of this invention is made in a molding process within a rigid mold capable of withstanding the internal forces caused by the pressure developed in the curing cycle.
- the composite structures of the head section 31 and the handle shaft 32 are wrapped individually to a tubular shell which is disposed in a mold cavity of the rigid mold.
- a solvent material such as methylene chloride or toluene etc., which is evaporable is provided or injected into each of the shells before the ends of the shells are closed.
- the solvent material which is in liquid state is freely disposed in the shell.
- the ends of the shell of the head section 31 contact the upper end of the shell of the handle shaft 32 and are coupled together by a plurality of layers of resin-impregnated graphite fibers arranged at 45 degrees to the longitudinal direction of the handle shaft, and preferable alternating between +45 and -45 degrees, as shown in dotted lines in FIG. 1.
- a reinforcement sheet 33 is preferably wrapped over the fiber sheets at the coupling portions of the ends of the shells.
- the solvent material is caused to evaporate or to expand from liquid state to gaseous state by the heat during the curing process.
- the solvent agent expands, it generates pressure within the confined mold cavity in order to bond together the graphite fiber layers into a unitary shell.
- the pressure which is generated by the vaporized solvent material is even and homogenous.
- the mold is cooled and then opened; and the molded frame is removed. Holes for strings are drilled in the head. Thereafter, the balance of the frame is checked and adjusted. The frame is painted and the strings are installed. A racket frame or excellent structural integrity is thus obtained.
- the racket frame has a hollow interior.
- the required mass of the solvent material is determined by the gas equation as follows:
- P is the pressure in each shell, (atm),
- V is the volume in each shell, (l)
- M is the molecular weight of the solvent material (gm/mole)
- R is the universal gas constant (0.082 atm-1/mole K)
- T is the absolute temperature (degree K)
- the inside volume of the racket frame V, the universal gas constant R and the molecular weight M of the solvent material to be used can be selected and predetermined. Therefore, when a required heating temperature T and pressure P for a curing process are selected, i.e., when the temperature and the pressure P are determined, the mass of the solvent material can be precisely calculated by this equation.
- the method in accordance with the present invention can produce a badminton racket frame of excellent structural integrity. No foamable materials are required.
- the badminton racket frame can be produced easily without a compressor which is required in a conventional method to generate a pressurized air in order to produce the racket frames.
- there is only about 2 grams of solvent material is required for manufacturing a badminton racket frame.
- the method is also suitable for manufacturing other objects which is made of composite materials, such as tennis racket.
- a continuous shell for both the head section 31 and the handle shaft 32 of the racket frame is prepared and arranged within the mold cavity. Both ends of the continuous shell are closed after the solvent material is inserted into the shell. An even and steady pressure which is generated by the vaporized solvent material is applied to the racket frame during curing stage.
- the handle shaft 32 of the racket frame is preshaped and cured before inserting into the mold cavity. Only the head section 31 is cured under the method as described above. In this case, only both ends of the shell of the head section are closed before they are wrapped together with the upper end of the handle shaft 32 which has already cured, and the shell is arranged within the mold cavity so that the solvent material is limited to vaporize within the shell of the head section.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
A method of producing a badminton racket frame includes the following steps. Prepare a mold cavity. Wrap a number of layers of graphite fibers so as to form a shell shaped in the form of the racket frame. Insert solvent material into the shell. Arrange the shell within the mold cavity. Heat the solvent material to cause expansion and to generate pressure within the mold cavity so as to press against the layers of graphite fibers and thereby provide intimate bonding of the layers. Remove the shell as an integral composite badminton racket frame.
Description
The present invention relates to a method, and more particularly to a method of producing a badminton racket frame.
There are two main processes which are widely used for making or producing tennis or badminton rackets in the world today. First of all, a comparison of the playing function and the racket property between a tennis racket and a badminton racket is listed in Table 1.
TABLE 1 ______________________________________ ITEM PLAYING FUNCTION RACKET PROPERTY ______________________________________ Bad- 1 Less momentum Vibration is careless min- 2 Ball travels at a Top frame should be ton lower speed when strong and rigid, the racket striking string tension should be as high as possible 3 Power comes Flexible and explosive mostly from the powerful shaft is player himself needed 4 Big deflection at Shaft should be durable the shaft during with stiffness equal on the play its both sides Tennis 1 More momentum Vibration is crucial Racket 2 Ball travels at a Strong frame and proper higher speed when flexibility on the yoke striking area could have a good rebound and com- fortable feeling 3 Power comes Comfortable condition mostly from the area essential, for response of instant: larger sweet- stroke spot, proper weight and balance for individual players ______________________________________
It is very important that different rackets which have different function requirements should be made by different manufacturing processes.
The first method employs a foamable material. The racket comprises a core which includes a foamable material or a foamable resin composition. U.S. Pat. No. 4,129,634 to Cecka et al. discloses a method for producing a racket frame which has a strip shaped foamable plastic core disposed therein. The strip of foamable material is maintained within a seamless sleeve made of a thin, flexible cellulosic film which is disposed in an outer shell forming the racket frame. The outer shell is disposed in a mold cavity. The foamable material is caused to expand and to generate pressure within the mold cavity and thereby provide intimate bonding of the core to the shell. It is very important that a steady and firm pressure is required to be applied to the frame during the curing stage. As shown in FIG. 4, the powder of foaming agent is blended into or added to the plastics carrier in order to form a strip of foamable material. Generally, the powder of foaming agent can not be blended evenly in the plastics carrier so that the strip of foamable material has a limited uniformity and may not be expanded or inflated uniformly or evenly. In addition, the racket frame which is made by the above-mentioned method with a core disposed therein has a weight heavier than the hollow racket frames.
The second method is an air injection method which employs a pressurized air injected into the racket frame. This is the most popular method used today to manufacture both badminton racket and tennis racket. As shown in FIG. 5, the composite structure of the tennis racket frame 20 includes a plurality of layers, each made of a sheet of composite fibers, unidirectionally oriented and resin-impregnated. The tennis racket frame 20 has a fluent and smooth passage 21 or hollow interior formed therein and has no sharp angles formed therein so that the pressurized air can be easily injected into the passage 21 of the racket frame 20 from one end of the passage 21. Therefore, the air injection method is suitable for manufacturing tennis racket frames.
As shown in FIG. 6, the composite structure of the badminton racket frame comprises a shell 10 including a plurality of layers, each made of a sheet of composite fibers, unidirectionally oriented and resin-impregnated. The shell 10 includes a head section 11 and a handle shaft 12 with a passage 14 formed therethrough. One end 15 of the shell 10 is closed. A sharp angle exists between the head section 11 and the handle shaft 12 or in the so called T-joint area. During a heating process and/or a compression process, a pressurized air is continuously injected into the passage 14 from the free end of the handle shaft 12 in order to expand the shell 10 which is arranged within a mold cavity. Occasionally, the pressurized air is jammed or obstructed in the sharp angle portion of the T-joint area, and may not flow through this portion swiftly. In addition, when the pressurized air is injected into the passage 14, the head section 11 inflates and the closed end 15 has a tendency to extend toward and to press the passage 14 of the shell 10, particularly the sharp angle area so that the angle area will further be obstructed. Therefore, because of the two deadly problems as mentioned above, about 25% of the products made by this method are rejected products and are unacceptable. Furthermore, a compressor or the like is required to produce and to provide the pressurized air.
The present invention has arisen to solve the afore-described disadvantages of the conventional method for producing badminton racket frames.
The primary objective of the present invention is to provide a method of producing a badminton racket frame which has an evaporable solvent disposed therein in order to generate a pressure within the racket frame so that the racket frame can be formed uniformly and homogeneously.
In accordance with one aspect of the invention, there is provided a method of producing a badminton racket frame which includes preparing a mold cavity shaped in the form of a badminton racket frame having a head section and a handle shaft. A number of layers of unidirectionally oriented resin-impregnated graphite fibers are wrapped so as to form a shell shaped in the form of the sections. Solvent material is inserted into the shell and the ends of the shell are closed. The wrapped shell is arranged within the mold cavity. The solvent material is heated to cause expansion and to generate pressure within the mold cavity so as to press against the layers of graphite fibers and thereby provide intimate bonding of the layers. The shell is removed as an integral composite badminton racket frame.
Further objectives and advantages of the present invention will become apparent from a careful reading of the detailed description provided hereinbelow, with appropriate reference to the accompanying drawings.
FIG. 1 is a schematic view of a badminton racket frame made by a method in accordance with the present invention;
FIG. 2 is an enlarged cross sectional view showing the composite structure of the badminton racket frame which has a plurality of successive layers serially exposed;
FIG. 3 is an enlarged view of a portion of the unidirectionally oriented resin-impregnated graphite fiber structure of the badminton racket frame, with successive layers serially exposed;
FIG. 4 is a schematic view illustrating the compositions of a strip of a foamable material;
FIG. 5 is a schematic view of a tennis racket frame made by a conventional air injection method; and
FIG. 6 is a schematic view of a badminton racket frame made by a conventional air injection method.
Referring to FIGS. 1, 2 and 3, the badminton racket frame in accordance with the present invention comprises a head section 31 and a handle shaft 32 with a grip affixed to the lower end of the handle shaft 32.
The structure of the racket frame is generally a shell comprising a plurality of layers 30, each made of a sheet of a so-called prepreg of composite material, or a unidirectionally oriented and resin-impregnated composite material, such as graphite fiber, boron fiber or glass fiber etc., in which most of the racket frames are made of graphite fibers. It is preferable that every two adjacent layers 30 are arranged at predetermined or suitable angles to each other, as shown in FIG. 3. The graphite fibers used to make the graphite fiber sheets comprises yarns containing hundreds, or thousands, of individual filaments, as is known in the art.
The composite structure of this invention is made in a molding process within a rigid mold capable of withstanding the internal forces caused by the pressure developed in the curing cycle. The composite structures of the head section 31 and the handle shaft 32 are wrapped individually to a tubular shell which is disposed in a mold cavity of the rigid mold. A solvent material, such as methylene chloride or toluene etc., which is evaporable is provided or injected into each of the shells before the ends of the shells are closed. The solvent material which is in liquid state is freely disposed in the shell. In the yoke area of the racket frame, the ends of the shell of the head section 31 contact the upper end of the shell of the handle shaft 32 and are coupled together by a plurality of layers of resin-impregnated graphite fibers arranged at 45 degrees to the longitudinal direction of the handle shaft, and preferable alternating between +45 and -45 degrees, as shown in dotted lines in FIG. 1. A reinforcement sheet 33 is preferably wrapped over the fiber sheets at the coupling portions of the ends of the shells.
The solvent material is caused to evaporate or to expand from liquid state to gaseous state by the heat during the curing process. As the solvent agent expands, it generates pressure within the confined mold cavity in order to bond together the graphite fiber layers into a unitary shell. The pressure which is generated by the vaporized solvent material is even and homogenous. Upon completion of the curing cycle, the mold is cooled and then opened; and the molded frame is removed. Holes for strings are drilled in the head. Thereafter, the balance of the frame is checked and adjusted. The frame is painted and the strings are installed. A racket frame or excellent structural integrity is thus obtained. The racket frame has a hollow interior.
It is very important to determine the required mass and/or the volume of the solvent material before it is injected into the shell. The required mass of the solvent material is determined by the gas equation as follows:
PV=nRT=(m/M)RT,
in which
P is the pressure in each shell, (atm),
V is the volume in each shell, (l)
n is the molecular number (moles), (n=m/M)
m is the mass of the solvent material (gm),
M is the molecular weight of the solvent material (gm/mole),
R is the universal gas constant (0.082 atm-1/mole K), and
T is the absolute temperature (degree K),
(T=273+ the heating temperature during curing process, degree C).
The inside volume of the racket frame V, the universal gas constant R and the molecular weight M of the solvent material to be used can be selected and predetermined. Therefore, when a required heating temperature T and pressure P for a curing process are selected, i.e., when the temperature and the pressure P are determined, the mass of the solvent material can be precisely calculated by this equation.
The following is an example for calculating the required mass of the solvent material:
the volume in a shell V=0.07 l, a selected curing temperature 150° C. (T=273+150K), a selected pressure in the shell P=10 atm, gas constant R=0.082 atm-1/mole K, and the molecular weight of a ethylene chloride M=97.0 gm/mole; therefore, according to the above-mentioned equation: m=PVM/RT=(10*0.07*97.0)/(0.082*423)=1.96 gm. Accordingly, the required mass of the solvent material can be precisely calculated.
Accordingly, the method in accordance with the present invention can produce a badminton racket frame of excellent structural integrity. No foamable materials are required. The badminton racket frame can be produced easily without a compressor which is required in a conventional method to generate a pressurized air in order to produce the racket frames. In addition, there is only about 2 grams of solvent material is required for manufacturing a badminton racket frame. The method is also suitable for manufacturing other objects which is made of composite materials, such as tennis racket.
Alternatively, a continuous shell for both the head section 31 and the handle shaft 32 of the racket frame, similar to the shell as shown in FIG. 6, is prepared and arranged within the mold cavity. Both ends of the continuous shell are closed after the solvent material is inserted into the shell. An even and steady pressure which is generated by the vaporized solvent material is applied to the racket frame during curing stage.
Further alternatively, the handle shaft 32 of the racket frame is preshaped and cured before inserting into the mold cavity. Only the head section 31 is cured under the method as described above. In this case, only both ends of the shell of the head section are closed before they are wrapped together with the upper end of the handle shaft 32 which has already cured, and the shell is arranged within the mold cavity so that the solvent material is limited to vaporize within the shell of the head section.
Although this invention has been described with a certain degree of particularity, it is to be understood that the present disclosure has been made by way of example only and that numerous changes in the detailed construction and the combination and arrangement of parts may be resorted to without departing from the spirit and scope of the invention as hereinafter claimed.
Claims (3)
1. A method of producing a badminton racket frame comprising preparing a mold cavity shaped in the form of said badminton racket frame having generally a head section and a handle shaft, wrapping a plurality of layers of unidirectional oriented resin-impregnated graphite fibers so as to form a first tubular shell shaped in the form of said handle shaft and a second tubular shell shaped in the form of said head section, inserting solvent material into said first shell and second shell, closing both ends of said first shell and said second shell, wrapping said ends of said second shell and an upper end of said first shell together by a plurality of layers of unidirectionally oriented resin-impregnated graphite fibers, arranging said wrapped first shell and said second shell within said mold cavity, heating said solvent material to cause expansion from the liquid state to the gaseous state and to generate pressure within said mold cavity so as to press against said layers of graphite fibers and thereby provide intimate bonding of said layers, and thereafter removing from said mold cavity said first shell and said second shell as an integral composite badminton racket frame.
2. A method of producing a badminton racket frame comprising preparing a mold cavity shaped in the form of said badminton racket frame having generally a head section and a handle shaft, wrapping a plurality of layers of unidirectionally oriented resin-impregnated graphite fibers so as to form a continuous tubular shell shaped in the form of said head section and said handle shaft, inserting solvent material into said continuous tubular shell, closing both ends of said continuous tubular shell, wrapping a yoke area of said shell by a plurality of layers of unidirectionally oriented resin-impregnated graphite fibers, arranging said wrapped continuous shell within said mold cavity, heating said solvent material to cause expansion from the liquid state to the gaseous state and to generate pressure within said mold cavity so as to press against said layers of graphite fibers and thereby provide intimate bonding of said layers, and thereafter removing from said mold cavity said continuous shell as an integral composite badminton racket frame.
3. A method of producing a badminton racket frame comprising preparing a mold cavity shaped in the form of said badminton racket frame having generally a head section and a handle shaft, preparing a first shell which has been cured and which has a shape in the form of said handle shaft, wrapping a plurality of layers of unidirectionally oriented resin-impregnated graphite fibers so as to form a second tubular shell shaped in the form of said head section, inserting solvent material into said second tubular shell, closing both ends of said second shell, wrapping said ends of said second shell and an upper end of said first shell together by a plurality of layers of unidirectionally oriented resin-impregnated graphite fibers, arranging said wrapped first shell and said second shell within said mold cavity, heating said solvent material to cause expansion from the liquid state to the gaseous state and to generate pressure within said mold cavity so as to press against said layers of graphite fibers of said second shell and thereby provide intimate bonding of said layers, and thereafter removing from said mold cavity said first shell and said second shell as an integral composite badminton racket frame.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US07/545,207 US5006298A (en) | 1990-06-28 | 1990-06-28 | Method of producing a badminton racket frame |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US07/545,207 US5006298A (en) | 1990-06-28 | 1990-06-28 | Method of producing a badminton racket frame |
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US5006298A true US5006298A (en) | 1991-04-09 |
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US07/545,207 Expired - Fee Related US5006298A (en) | 1990-06-28 | 1990-06-28 | Method of producing a badminton racket frame |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5238247A (en) * | 1992-03-12 | 1993-08-24 | Prince Manufacturing, Inc. | Mono-shaft sports racquet |
US5344139A (en) * | 1993-11-09 | 1994-09-06 | Jan Sports Products Corp. | Racket shaft mounting device |
US5417418A (en) * | 1992-12-10 | 1995-05-23 | Prince Manufacturing, Inc. | Monoshaft composite tennis racquet |
US5766539A (en) * | 1994-01-21 | 1998-06-16 | Yamaha Corporation | Process of molding racket frame formed of fiber reinforced thermoplastic resin free from burr and burn |
US20070054761A1 (en) * | 2005-09-03 | 2007-03-08 | Wilson Sporting Goods Co. | Reinforcing member for a badminton racquet |
US20090215557A1 (en) * | 2008-02-22 | 2009-08-27 | Pick-A-Paddle, Inc. | Institutional badminton racket |
US20110136602A1 (en) * | 2009-06-18 | 2011-06-09 | Xene Corporation | Fiber composite and process of manufacture |
TWI385013B (en) * | 2009-06-12 | 2013-02-11 | ||
EP3753700A1 (en) * | 2019-06-21 | 2020-12-23 | Marshal Industrial Corp. | Method of manufacturing a composite rim |
US11020879B2 (en) * | 2018-05-17 | 2021-06-01 | Sikorsky Aircraft Corporation | Self pressurizing bladder tooling |
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US11020879B2 (en) * | 2018-05-17 | 2021-06-01 | Sikorsky Aircraft Corporation | Self pressurizing bladder tooling |
US11618184B2 (en) | 2018-05-17 | 2023-04-04 | Sikorsky Aircraft Corporation | Self pressurizing bladder tooling |
US11839997B2 (en) | 2018-05-17 | 2023-12-12 | Sikorsky Aircraft Corporation | Self pressurizing bladder tooling |
EP3753700A1 (en) * | 2019-06-21 | 2020-12-23 | Marshal Industrial Corp. | Method of manufacturing a composite rim |
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